EP0924420B1 - Régulateur de couple pour un moteur à combustion interne - Google Patents
Régulateur de couple pour un moteur à combustion interne Download PDFInfo
- Publication number
- EP0924420B1 EP0924420B1 EP98123769A EP98123769A EP0924420B1 EP 0924420 B1 EP0924420 B1 EP 0924420B1 EP 98123769 A EP98123769 A EP 98123769A EP 98123769 A EP98123769 A EP 98123769A EP 0924420 B1 EP0924420 B1 EP 0924420B1
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- EP
- European Patent Office
- Prior art keywords
- combustion
- engine
- target
- fuel
- intake air
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D43/00—Conjoint electrical control of two or more functions, e.g. ignition, fuel-air mixture, recirculation, supercharging or exhaust-gas treatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/18—Circuit arrangements for generating control signals by measuring intake air flow
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/3011—Controlling fuel injection according to or using specific or several modes of combustion
- F02D41/3017—Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used
- F02D41/3023—Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used a mode being the stratified charge spark-ignited mode
- F02D41/3029—Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used a mode being the stratified charge spark-ignited mode further comprising a homogeneous charge spark-ignited mode
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D2041/389—Controlling fuel injection of the high pressure type for injecting directly into the cylinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/04—Engine intake system parameters
- F02D2200/0402—Engine intake system parameters the parameter being determined by using a model of the engine intake or its components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/10—Parameters related to the engine output, e.g. engine torque or engine speed
- F02D2200/1002—Output torque
- F02D2200/1004—Estimation of the output torque
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/10—Parameters related to the engine output, e.g. engine torque or engine speed
- F02D2200/1006—Engine torque losses, e.g. friction or pumping losses or losses caused by external loads of accessories
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2250/00—Engine control related to specific problems or objectives
- F02D2250/18—Control of the engine output torque
Definitions
- the present invention is directed to a torque controller and to a method for controlling an intake air quantity of an internal combustion engine.
- the invention is directed to a torque controller for an internal combustion engine by controlling intake air quantity based on a state of combustion.
- JP 09-287513 A there is known an apparatus for controlling a torque produced from an internal combustion engine operable at an air/fuel ratio, wherein in operation of the engine, fuel is injected to and mixed with intake air prior entering the combustion chamber.
- the engine torque control apparatus includes a first control device for controlling an amount of air permitted to enter the engine, and a second control device for controlling an amount of fuel metered to the engine.
- Target values for the engine torque and air/fuel ratio are calculated based on the sensed engine operating conditions.
- the first and second control devices are set to control the engine torque to the target value calculated therefor and the air/fuel ratio to the target value calculated therefor.
- a target opening degree of an electronic controlled throttle valve is calculated from a lookup table, which defines the target throttle position as a function of target engine torque and engine rotation.
- the conventional practice is made on an assumption that the air/fuel ratio is fixed at a predetermined value, for example, at the stoichiometric an/fuel ratio. Therefore, in this case, the lookup table which defines the target opening degree of the throttle valve has settings suitable for the stoichiometric air/fuel ratio. Thus, the conventional practice cannot be applied to the engine which changes the air/fuel ratio according to engine operating conditions.
- fuel is injected during an intake stroke to diffuse the injected fuel so as to form a homogeneous mixture in the combustion chamber.
- fuel is injected during a compression stroke to form a stratified fuel mixture around a spark plug.
- the air/fuel ratio around the spark plug is also 25.
- the air/fuel ratio around the spark plug is much less, for example 10, since the air/fuel ratio around the spark plug is very rich, fuel is concentrated around the spark plug. This results in the combustion efficiency in the stratified combustion being worse than in the homogeneous combustion. In short, the combustion efficiency is different according to the state of combustion.
- the target opening degree of the throttle valve is corrected based on the air/fuel ratio, the target engine torque cannot be achieved accurately. Also a torque difference occurs when the state of combustion changes, for example, when the combustion mode changes between the homogeneous combustion and the stratified combustion.
- a torque controller for a direct-injection type internal combustion engine which can achieve the target engine torque, without being affected by the combustion mode.
- a torque controller for an internal combustion engine which can achieve the target engine torque, without being affected by change of the combustion mode between the homogeneous combustion and the stratified combustion.
- Fig. 1 is a system diagram showing a direct-injection type gasoline internal combustion engine.
- a multi-cylinder engine 10 for a vehicle includes a combustion chamber 11 and a cylinder 12.
- a piston 13, which reciprocates in the cylinder 12, has a shallow bowl 14 on the piston crown 15 in order to accomplish a stratified combustion and a homogeneous combustion.
- the stratified combustion and the homogeneous combustion are explained in detail later.
- Intake air is introduced from an air cleaner 16 through an intake passage 17, an intake manifold 18, and an intake port 19 to the cylinder 12. Intake air quantity is controlled by a throttle valve 20, which is provided in the intake passage 17.
- the throttle valve 20 is actuated by an actuator 21, for example, a step motor operable in response to a drive signal outputted from a control unit 50.
- An electro-magnetic fuel injector 22 which injects fuel directly into the combustion chamber 11, is disposed to provide fuel to each cylinder 12.
- the fuel injector 22 injects fuel when its solenoid receives a fuel injection pulse signal outputted from the control unit 50.
- the spark plug 23, for igniting the mixture in the combustion chamber 11, is mounted at the center of the cylinder 12.
- a spark timing is controlled by the control unit 50 based on the engine operating conditions.
- the combustion modes include the homogeneous stoichiometric combustion mode, the homogeneous lean combustion mode, and the stratified lean combustion mode, in accordance with the air/fuel ratio control.
- the homogeneous lean combustion is operated at air/fuel ratio ranging from about 20 to 30, and the stratified lean combustion is operated at air/fuel ratio of about 40.
- the region of combustion mode is defined basically based on a target equilibrium engine torque and an engine rotation.
- an exhaust gas from the combustion chamber 11 is discharged into an exhaust passage 24.
- the exhaust passage 24 has a catalytic converter 25 for purifying the exhaust gas.
- the control unit 50 includes a microcomputer comprised of a CPU, a ROM, a RAM, an A/D converter and an input/output interface.
- a microcomputer comprised of a CPU, a ROM, a RAM, an A/D converter and an input/output interface.
- the sections described herein are implemented in hardware, software, or a combination of both, in the control unit.
- the control unit 50 receives signals from various sensors. These sensors include an accelerator sensor 26 for detecting an accelerator pedal position APS of an accelerator pedal 27; a coolant temperature sensor 28 for detecting the temperature Tw of the coolant of the engine; an O 2 sensor 29 positioned in the exhaust passage 24 for producing a signal corresponding to the rich/lean composition of the exhaust gas for actual air/fuel ratio determination; and vehicle speed sensor 30 for detecting the vehicle speed VSP.
- sensors include an accelerator sensor 26 for detecting an accelerator pedal position APS of an accelerator pedal 27; a coolant temperature sensor 28 for detecting the temperature Tw of the coolant of the engine; an O 2 sensor 29 positioned in the exhaust passage 24 for producing a signal corresponding to the rich/lean composition of the exhaust gas for actual air/fuel ratio determination; and vehicle speed sensor 30 for detecting the vehicle speed VSP.
- the sensors also include an air flow meter 31 provided in the intake passage 17 at a position upstream of the throttle valve 20 for detecting an intake air rate Qa; a throttle sensor 32, including an idle switch positioned to be turned on when the throttle valve 20 is fully closed, for detecting a throttle opening degree TVO of throttle valve 20; and angle sensors 33 and 34 (engine rotation sensor) for detecting a rotation of a crankshaft or camshaft of the engine 10.
- an air flow meter 31 provided in the intake passage 17 at a position upstream of the throttle valve 20 for detecting an intake air rate Qa
- a throttle sensor 32 including an idle switch positioned to be turned on when the throttle valve 20 is fully closed, for detecting a throttle opening degree TVO of throttle valve 20
- angle sensors 33 and 34 engine rotation sensor
- the sensors 33 and 34 produce a reference pulse signal REF and a unit pulse signal POS.
- the REF is outputted at every 720°/n of rotation of the crankshaft (where n is the number of cylinders). For example, in a four-cylinder engine, the REF is output at every 180° of rotation of the crankshaft.
- the POS is outputted at every 1 degree of rotation of the crankshaft.
- the control unit 50 calculates an engine rotation Ne based on the signal outputted from the sensors 33 and 34.
- the control unit 50 receives the signals fed thereto from the various sensors and includes a microcomputer built therein for making the calculations described herein to control the opening degree of the electronic controlled throttle valve 20, the amount and timing of fuel injected to the engine by fuel injector 22, and spark timing of the spark plug 23.
- Fig. 2 shows the calculation of a target throttle position and a fuel injection pulse.
- An equilibrium engine torque tTEO is calculated from a lookup table, as shown in a block A of Fig. 2.
- the lookup table which may be obtained experimentally (e.g., from tests performed by the manufacturer), specifies the equilibrium engine torque tTEO (target engine torque) as a function of accelerator pedal position APS and engine rotation Ne.
- the accelerator pedal position APS corresponds to the operator's demanded engine load or torque.
- a target intake air flow rate TTPO which corresponds to a ratio of reference air/fuel ratio (stoichiometric air/fuel ratio), is calculated from a lookup table, as shown in a block B of Fig. 2.
- the lookup table which may be obtained experimentally (e.g., from tests performed by the manufacturer), specifies the target intake air flow rate TTPO as a function of engine rotation Ne and equilibrium engine torque tTEO calculated in the block A.
- An intake air quantity introduced into the engine during each intake stroke can be used instead of the target intake air flow rate TTPO.
- a basic fuel injection pulse width corresponding to the intake air quantity introduced into the engine during each intake stroke or the intake air quantity detected by air flow meter 31 every unit time can be used instead of the target intake air flow rate TTPO.
- a target equivalent ratio tDML which corresponds to the ratio of the reference air/fuel ratio (stoichiometric) with respect to the target ratio of air and fuel, is calculated from a lookup table, as shown in a block C of Fig. 2.
- the lookup table which may be obtained experimentally (e.g., from tests performed by the manufacturer), defines the target equivalent ratio tDML as a function of accelerator pedal position APS and engine rotation Ne.
- the combustion modes include the homogeneous stoichiometric combustion mode, the homogeneous lean combustion mode, and the stratified lean combustion mode. Therefore, it is determined in the block C which combustion mode is operated, and the target equivalent ratio tDML is set within the predetermined range of determined combustion mode.
- the target equivalent ratio tDML may be corrected by using one of the following factors or by combining more than one of the following factors; the coolant temperature Tw; the vehicle speed VSP; the acceleration of the vehicle; the elapsed time after the engine starting; the negative pressure of a break booster; and the load of an auxiliary machine (such as an alternator during idling condition).
- the produced engine torque is different between the homogeneous combustion and the stratified combustion, even if the air/fuel ratio is the same.
- the homogeneous combustion and the stratified combustion can be operated at the same air/fuel ratio when the combustion mode changes.
- the combustion mode changes based on a target equilibrium engine torque and an engine rotation.
- the target equilibrium engine torque changes into the direction of the arrow in Fig. 10
- the combustion mode changes from the stratified lean combustion to the homogeneous lean combustion.
- the throttle valve is controlled to the shutting direction, and the equivalent ratio continuously increases corresponding to the decreasing of the intake air quantity.
- the equivalent ratio crosses a rich limit of the stratified combustion (a lean limit of the homogeneous combustion)
- the stratified lean combustion and the homogeneous lean combustion can be operated at the same air/fuel ratio.
- a combustion efficiency correction rate ITAF corresponding to each combustion is calculated from lookup tables, as shown in a block D of Fig. 2.
- lookup tables which may be obtained experimentally (e.g., from computer-simulated data or from actual tests performed on vehicles), define the combustion efficiency correction rate ITAF as a function of target equivalent ratio tDML.
- a combustion mode signal which shows whether the combustion mode (combustion state) is in the stratified combustion or in the homogeneous combustion, is inputted to the block D.
- the combustion mode signal is generated in the block C.
- the target equivalent ratio tDML is also inputted to the block D.
- the combustion efficiency correction rate ITAF is calculated from the lookup table provided for the stratified combustion with the target equivalent ratio tDML used in table lookup.
- the combustion efficiency correction rate ITAF is calculated from the lookup table provided for the homogeneous combustion with the target equivalent ratio tDML used in the table lookup.
- the control unit 50 calculates a target intake air flow rate TTP1 by multiplying the target intake air flow rate TTPO calculated in block B with the combustion efficiency correction rate ITAF calculated in block D. Following the calculation of the target intake air flow rate TTP1, the control unit 50 calculates an eventual target intake air flow rate TTP2 by dividing the calculated target intake air flow rate TTP1 by the target equivalent ratio tDML calculated in block C. The eventual target intake air flow rate TTP2 corresponds to the target engine torque at the target air/fuel ratio and at the operated combustion state.
- the combustion efficiency correction rate ITAF is defined as a fuel economy rate at the reference air/fuel ratio (stoichiometric) divided by a fuel economy rate for each air/fuel ratio.
- the combustion efficiency correction rate ITAF for the homogeneous combustion mode at the point B is defined as b/a
- the combustion efficiency correction rate ITAF for the stratified combustion mode at the point E is defined as e/a. Therefore, the combustion efficiency correction rate ITAF is equal to 1 at the reference air/fuel ratio (14.6), and the combustion efficiency correction rate ITAF is less than 1 when the air/fuel ratio is lean as compared to the reference air/fuel ratio.
- the target equivalent ratio tDML is defined as the reference air/fuel ratio (stoichiometric) divided by each air/fuel ratio.
- the target equivalent ratio tDML is equal to 1 when the target air/fuel ratio is stoichiometric, and the target equivalent ratio tDML is equal to 0.5 when the target air/fuel ratio is 29.2.
- the target intake air flow rate TTPO is corrected by the target equivalent ratio tDML after correction by the combustion efficiency correction rate ITAF, alternatively, it may be also possible that the target intake air flow rate TTPO is corrected by the combustion efficiency correction rate ITAF after correction by the target equivalent ratio tDML.
- a target throttle valve position TTPS is calculated from a lookup table, as shown in a block E of Fig. 2.
- the lookup table which may be obtained experimentally (e.g., from tests performed by the manufacturer), defines the target throttle valve position TTPS as a function of eventual target intake air flow rate TTP2 and engine rotation Ne.
- the calculated target throttle valve position TTPS is transferred to the actuator 21, which thereby moves the throttle valve 20 to the target throttle valve position TTPS so as to achieve the eventual target intake air flow rate TTP2.
- a basic fuel injection pulse width Tp (in units of msec) is calculated in the block F of Fig. 2.
- an eventual fuel injection pulse width Ti (in units of msec) is calculated, as shown in the block G of Fig. 2.
- the calculated eventual fuel injection pulse width Ti is transferred to the fuel injector 22 so as to inject fuel in such an amount as to achieve the target air/fuel ratio.
- Fig. 3 is a flow diagram, which shows the process for controlling the block diagram of Fig. 2.
- step S1 which corresponds to the block A of Fig. 2, the equilibrium engine torque tTEO is calculated based on the accelerator pedal position APS and the engine rotation Ne.
- step S2 which corresponds to the block C of Fig. 2, the target equivalent ratio tDML is calculated based on the accelerator pedal position APS and the engine rotation Ne.
- the target intake air flow rate TTPO is calculated based on the equilibrium engine torque tTEO calculated in the step S1 and the engine rotation Ne.
- step S4 it is determined whether the combustion mode (combustion state) is in the stratified combustion or in the homogeneous combustion.
- the routine proceeds to a step S5, and the combustion efficiency correction rate ITAF for the stratified combustion is calculated based on the target equivalent ratio tDML.
- the routine proceeds to a step S6, and the combustion efficiency correction rate ITAF for the homogeneous combustion is calculated based on the target equivalent ratio tDML.
- the target intake air flow rate TTP1 is calculated by the following equation (1), where TTPO is the target intake air flow rate calculated in the step S3, and ITAF is the combustion efficiency correction rate calculated in the step S5 or S6.
- TTP ⁇ 1 TTPO ⁇ ITAF
- the target intake air flow rate TTP1 is corrected by the combustion efficiency correction rate ITAF, the target engine torque can be achieved accurately without being affected by the difference of combustion state. Also, a torque difference does not occur even though the combustion mode changes between the homogeneous combustion and the stratified combustion.
- the eventual target intake air flow rate TTP2 which corresponds to the target equivalent ratio tDML, is calculated by the following equation (2), where TTP1 is the target intake air flow rate calculated in the step S7, and tDML is the target equivalent ratio calculated in the step S2.
- TTP ⁇ 2 TTP ⁇ 1 / tDML
- step S9 which corresponds to the block E of Fig. 2, the target throttle valve position TTPS is calculated based on the eventual target intake air flow rate TTP2 and engine rotation Ne.
- the calculated target throttle valve position TTPS is outputted to the actuator 21 of the throttle valve 20, so as to achieve the eventual target intake air flow rate TTP2.
- step S12 the calculated eventual fuel injection pulse width Ti is outputted to the injector 22 according to the predetermined timing which corresponds to the homogeneous combustion or the stratified combustion.
- the target throttle valve position is calculated as shown in Fig. 4.
- the basic composition is similar to that as shown in Fig. 1.
- the correction to the target intake air flow rate TTPO with the target equivalent ratio tDML and the combustion efficiency correction rate ITAF is different from the block diagram of Fig. 2.
- the other blocks are the same as the Fig. 2. Therefore, the other blocks are given the same reference characters as in Fig. 2, and the explanation is not repeated for sake of brevity and clarity.
- the control unit 50 calculates the target equivalent ratio tDML and the combustion efficiency correction rate ITAF. Following this calculation, a collection value to the target intake air flow rate TTPO is calculated by dividing the target equivalent ratio tDML by the combustion efficiency correction rate ITAF. Next, the eventual target intake air flow rate TTP2 is calculated by multiplying the target intake air flow rate TTPO with the calculated collection value.
- a correction with the target equivalent ratio tDML and the correction with the combustion efficiency correction rate ITAF are done to the target intake air flow rate TTPO at the same time.
- the third embodiment (which is not covered by the present invention) will be described with reference to the block diagram of Fig. 5 and the flow diagram of Fig. 6.
- the basic composition is similar to that as shown in Fig. 1.
- Fig. 5 shows the calculation of a target throttle valve position and a fuel injection pulse.
- the block H is added to the block diagram of Fig. 2, and the correction order to the target intake air flow rate TTPO with the target equivalent ratio tDML and the combustion efficiency correction rate ITAF is different from the block diagram of Fig. 2.
- a pumping loss torque TpI which corresponds to the target equivalent ratio, is calculated from a lookup table, as shown in the block H of Fig. 5.
- the lookup table which may be obtained experimentally (e.g., from tests performed by the manufacturer), defines the pumping loss torque TpI as a function of target equivalent ratio tDML.
- the pumping loss torque TpI is defined as a function of target equivalent ratio tDML is, as shown in Fig. 14, the pumping loss torque TpI becomes small by shifting the air/fuel ratio to lean. As the lean combustion involves a larger quantity of intake air under the same operating condition, the throttle valve can be opened to reduce the pumping loss. Therefore, the control unit 50 calculates a equilibrium engine torque TTC by adding the pumping loss torque TpI to the equilibrium engine torque tTEO calculated in the block A.
- the target intake air flow rate TTPO which corresponds to a ratio of reference air/fuel ratio (stoichiometric), is calculated from a lookup table, as shown in a block B' of Fig. 5.
- the lookup table which may be obtained experimentally (e.g., from tests performed by the manufacturer), specify the target intake air flow rate TTPO as a function of engine rotation Ne and equilibrium engine torque TTC corrected by the pumping loss torque TpI.
- the control unit 50 calculates a target intake air flow rate TTP1 by dividing the target intake air flow rate TTPO by the target equivalent ratio tDML calculated in block C. Following the calculation of the target intake air flow rate TTP1, the control unit 50 calculates an eventual target intake air flow rate TTP2 by multiplying the target intake air flow rate TTP1 with the combustion efficiency correction rate ITAF calculated in block D. Next, based on the calculated eventual target intake air flow rate TTP2, the target throttle valve position TTPS is calculated in block E.
- Fig. 6 is a flow diagram, which shows the process for controlling the block diagram of Fig. 5.
- step S21 which corresponds to the block A of Fig. 5, the equilibrium engine torque tTEO is calculated based on the accelerator pedal position APS and the engine rotation Ne.
- step S22 which corresponds to the block C of Fig. 5, the target equivalent ratio tDML is calculated based on the accelerator pedal position APS and the engine rotation Ne.
- step S23 which corresponds to the block H of Fig. 5, the pumping loss torque TpI is calculated based on the target equivalent ratio tDML.
- the equilibrium engine torque TTC is calculated by the following equation (3), where tTEO is the equilibrium engine torque calculated in the step S21, and TpI is the pumping loss torque calculated in the step S23.
- TTC tTEO + TpI
- the target intake air flow rate TTPO is calculated based on the equilibrium engine torque TTC calculated in the step S24 and the engine rotation Ne.
- the eventual target intake air flow rate TTP1 which corresponds to the target equivalent ratio, is calculated by the following equation (4), where TTP0 is the target intake air flow rate calculated in the step S25, and tDML is the target equivalent ratio calculated in the step S22.
- TTP ⁇ 1 TTP ⁇ 0 / tDML
- a step S27 it is determined whether the combustion mode (combustion state) is in the stratified combustion or in the homogeneous combustion.
- the routine proceeds to a step S28, and the combustion efficiency correction rate ITAF for the stratified combustion is calculated based on the target equivalent ratio tDML.
- the routine proceeds to a step S29, and the combustion efficiency correction rate ITAF for the homogeneous combustion is calculated based on the target equivalent ratio tDML.
- the target intake air flow rate TTP2 is calculated by the following equation (5), where TTP1 is the target intake air flow rate calculated in the step S26, and ITAF is the combustion efficiency correction rate calculated in the step S28 or S29.
- TTP ⁇ 2 TTP ⁇ 1 ⁇ ITAF
- step S31 which corresponds to the block E of Fig. 5
- the target throttle valve position TTPS is calculated based on the eventual target intake air flow rate TTP2 and the engine rotation Ne.
- the calculated target throttle valve position TTPS is outputted to the actuator 21 of the throttle valve 20, so as to achieve the eventual target intake air flow rate TTP2.
- a step S43 the calculated eventual fuel injection pulse width Ti is outputted to the injector 22 according to the predetermined timing which corresponds to the homogeneous combustion or the stratified combustion.
- the fourth embodiment will be described with reference to the block diagram of Fig. 7 and the flow diagram of Fig. 8.
- the basic composition is similar to that as shown in Fig. 1.
- Fig. 7 shows the calculation of a target throttle valve position and a fuel injection pulse.
- a block I is added to the block diagram of Fig. 2, and a block D' is modified from the block D of Fig. 2.
- the other blocks are the same as the block diagram of Fig. 2. Therefore, those other blocks are given the same reference characters as in Fig. 2, and the explanation of those blocks is not repeated for sake of brevity and clarity.
- the combustion efficiency correction rate ITAF is calculated from a lookup table, as shown in a block D' of Fig. 7.
- the lookup table which may be obtained experimentally (e.g., from computer-simulated data or from a fuel tests performed on vehicles), defines the combustion efficiency correction rate ITAF as a function of target equivalent ratio tDML. Comparing with the block D of Fig. 2, since there is only one lookup table, the data storage capacity of the control unit 50 is reduced.
- a combustion mode signal which shows whether the combustion mode (combustion state) is in the stratified combustion or in the homogeneous combustion, is inputted to the block I of Fig. 7.
- the block I switches a gain based on the combustion mode signal.
- the block I outputs a Gain, which corrects the combustion efficiency correction rate ITAF so as to be suited for the stratified combustion when the combustion mode is in the stratified combustion.
- the block I outputs 1 as the Gain.
- the combustion efficiency correction rate ITAF is corrected by multiplying it with the Gain. With this result, when the combustion mode is in the stratified combustion, the combustion efficiency correction rate ITAF calculated in the block D' of Fig. 7 is converted to a suitable value for the stratified combustion. When the combustion mode is in the homogeneous combustion, the combustion efficiency correction rate ITAF calculated in the block D' of Fig. 7 is outputted as it is.
- the lookup table in the block D' defines the combustion efficiency correction rate ITAF as a function of target equivalent ratio tDML (target air/fuel ratio) in entire range of the engine. Moreover, in the region where the combustion mode changes, the combustion efficiency correction rate ITAF is suited for homogeneous combustion. Therefore, the combustion efficiency correction rate ITAF is corrected by multiplying by the Gain (>1) when the combustion mode is in the stratified combustion.
- the Gain can be a fixed value or it can be a changeable value. However, a fixed value is preferable to reduce the capacity of the memory.
- Fig. 8 is a flow diagram, which shows the process for controlling the block diagram of Fig. 7.
- step S51 which corresponds to the block A of Fig. 7, the equilibrium engine torque tTEO is calculated based on the accelerator pedal position APS and the engine rotation Ne.
- step S52 which corresponds to the block C of Fig. 7, the target equivalent ratio tDML is calculated based on the accelerator pedal position APS and the engine rotation Ne.
- step S53 which corresponds to the block B of Fig. 7, the target intake air flow rate TTPO is calculated based on the equilibrium engine torque tTEO calculated in the step S51 and the engine rotation Ne.
- step S54 which corresponds to the block D' of Fig. 7, the combustion efficiency correction rate ITAF is calculated based on the target equivalent ratio tDML calculated in the step S52.
- step S55 it is determined whether the combustion mode (combustion state) is in the stratified combustion or in the homogeneous combustion based on the combustion mode signal.
- the routine proceeds to a step S56, and the Gain (>1) for the stratified combustion is selected.
- the combustion efficiency correction rate ITAF' is calculated by the following equation (6), where ITAF is the combustion efficiency correction rate calculated in the step S54, and Gain is the gain selected in the step S56 or S57.
- ITAF ⁇ ITAF ⁇ Gain
- the target intake air flow rate TTP1 is calculated by the following equation (7), where TTPO is the target intake air flow rate calculated in the step S53, and ITAF' is the combustion efficiency correction rate calculated in the step S58.
- TTP ⁇ 1 TTPO ⁇ ITAF ⁇
- the eventual target intake air flow rate TTP2 which corresponds to the target equivalent ratio tDML, is calculated by the following equation (8), where TTP1 is the target intake air flow rate calculated in the step S59, and tDML is the target equivalent ratio calculated in the step S52.
- TTP ⁇ 2 TTP ⁇ 1 / tDML
- step S61 which corresponds to the block E of Fig. 7, the target throttle valve position TTPS is calculated based on the eventual target intake air flow rate TTP2 and the engine rotation Ne.
- the calculated target throttle valve position TTPS is outputted to the actuator 21 of the throttle valve 20, so as to achieve the eventual target intake air flow rate TTP2.
- step S64 the calculated eventual fuel injection pulse width Ti is outputted to the injector 22 according to the predetermined timing which corresponds to the homogeneous combustion or the stratified combustion.
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- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Claims (9)
- Régulateur de couple qui contrôle une quantité d'air d'admission d'un moteur à combustion interne,
caractérisé en ce qu'il comprend:un détecteur pour détecter un régime de fonctionnement du moteur comprenant le fait qu'un mode de combustion du moteur est dans un mode de combustion homogène ou dans un mode de combustion stratifiée,une partie de calcul comprenant une partie de calcul de la quantité d'air d'admission cible pour calculer la quantité d'air d'admission cible (TTPO) en se basant sur le régime de fonctionnement du moteur, et un ratio cible de la partie de calcul d'air et de carburant pour calculer le ratio cible d'air et de carburant (tDML) en se basant sur ledit régime de fonctionnement du moteur,une partie de calcul du taux de correction du rendement de combustion pour calculer un taux de correction du rendement de combustion (ITAF) en se basant sur le mode de combustion du moteur et le ratio cible d'air et de carburant (tDML),une partie de correction pour corriger la quantité d'air d'admission cible (TTPO) en se basant sur le taux de correction du rendement de combustion (ITAF) et le ratio cible d'air et de carburant (tDML), dans laquelle la partie de correction comprend un tableau stockant des données qui définit le taux de correction du rendement de combustion (ITAF) comme une fonction du ratio cible d'air et de carburant (tDML), et une partie de commutation de gain (I) pour commuter un gain en se basant sur le mode de combustion du moteur, dans lequel le taux de correction du rendement de combustion (ITAF) calculé à partir du tableau est corrigé par le gain. - Régulateur de couple selon la revendication 1, caractérisé en ce que le détecteur comprend en outre un capteur de rotation du moteur (33, 34) pour détecter une rotation du moteur (Ne) et un capteur d'accélérateur (26) pour détecter une position de la pédale d'accélérateur (APS), dans lequel la partie de calcul de la quantité d'air d'admission cible calcule la quantité d'air d'admission cible (TTPO) en se basant sur la rotation du moteur (Ne) et la position de la pédale d'accélérateur (APS), et dans lequel le ratio cible de la partie de calcul d'air et de carburant calcule le ratio cible d'air et de carburant (tDML) en se basant sur la rotation du moteur (Ne) et la position de la pédale d'accélérateur (APS).
- Régulateur de couple selon la revendication 1 ou 2, caractérisé en ce que la partie de correction corrige la quantité d'air d'admission cible (TTPO) en utilisant le taux de correction du rendement de combustion (JTAF) et le ratio cible d'air et de carburant (tDML) dans un ordre particulier.
- Régulateur de couple selon l'une des revendications 1 à 3, caractérisé en ce que le moteur (10) comprend un injecteur (22) qui injecte du carburant directement dans la chambre de combustion (11) du moteur (10), dans lequel l'injecteur (22) injecte du carburant durant une course d'admission lorsque le mode de combustion est dans le mode de combustion homogène, et injecte du carburant durant une course de compression lorsque le mode de combustion est dans le mode de combustion stratifiée.
- Régulateur de couple selon l'une des revendications 1 à 4, caractérisé en ce que la partie de correction comprend des tableaux stockant des données, lesquels définissent le taux de correction du rendement de combustion respectivement pour le mode de combustion homogène et pour le mode de combustion stratifiée comme une fonction du ratio cible d'air et de carburant.
- Régulateur de couple selon l'une des revendications 1 à 5, caractérisé en ce que le tableau définit le taux de correction du rendement de combustion sur une plage entière du ratio cible d'air et de carburant du moteur.
- Régulateur de couple selon l'une des revendications 1 à 6, caractérisé par une partie de calcul du couple au niveau de la perte lors du pompage pour calculer un couple au niveau de la perte lors du pompage du moteur, dans lequel la partie de calcul de la quantité d'air d'admission cible calcule une quantité d'air d'admission cible en se basant sur le régime de fonctionnement du moteur et le couple au niveau de la perte lors du pompage du moteur.
- Régulateur de couple selon la revendication 7, caractérisé en ce que le couple au niveau de la perte lors du pompage du moteur est calculé en se basant sur le ratio cible d'air et de carburant.
- Procédé pour réguler une quantité d'air d'admission d'un moteur à combustion interne, comprenant les étapes consistant à :détecter un régime de fonctionnement du moteur comprenant le fait qu'un mode de combustion du moteur est dans un mode de combustion homogène ou dans un mode de combustion stratifiée,calculer une quantité d'air d'admission cible (TTPO) et un ratio cible d'air et de carburant (tDML) en se basant sur le régime de fonctionnement du moteur,calculer un taux de correction du rendement de combustion (ITAF) en se basant sur le mode de combustion du moteur et le ratio cible d'air et de carburant (tDML),corriger la quantité d'air d'admission cible (TTPO) en se basant sur le taux de correction du rendement de combustion (ITAF) et le ratio cible d'air et de carburant (tDML), dans lequel la quantité d'air d'admission cible (TTPO) est corrigée en se référant à un tableau stockant des données, lequel définit le taux de correction du rendement de combustion (ITAF) comme une fonction du ratio cible d'air et de carburant (tDML), et commuter un gain en se basant sur le mode de combustion du moteur, dans lequel le taux de correction du rendement de combustion (ITAF) calculé à partir du tableau est corrigé par le gain.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP34514497 | 1997-12-15 | ||
JP9345144A JPH11182299A (ja) | 1997-12-15 | 1997-12-15 | エンジンのトルク制御装置 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0924420A2 EP0924420A2 (fr) | 1999-06-23 |
EP0924420A3 EP0924420A3 (fr) | 2000-09-13 |
EP0924420B1 true EP0924420B1 (fr) | 2007-02-28 |
Family
ID=18374587
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98123769A Expired - Lifetime EP0924420B1 (fr) | 1997-12-15 | 1998-12-14 | Régulateur de couple pour un moteur à combustion interne |
Country Status (4)
Country | Link |
---|---|
US (1) | US6145489A (fr) |
EP (1) | EP0924420B1 (fr) |
JP (1) | JPH11182299A (fr) |
DE (1) | DE69837189T2 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9284897B2 (en) | 2012-08-31 | 2016-03-15 | Honda Motor Co., Ltd. | Intake control system for internal combustion engine |
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FR2757945B1 (fr) * | 1996-12-27 | 1999-02-05 | Renault | Procede de calcul du couple d'un moteur thermique a injection commandee electroniquement |
SE521717C2 (sv) * | 1999-07-05 | 2003-12-02 | Volvo Personvagnar Ab | Förfarande för styrning av förbränningsmotor, samt arrangemang för sådant förfarande |
FR2796670B1 (fr) * | 1999-07-23 | 2001-10-26 | Peugeot Citroen Automobiles Sa | Procede et dispositif de commande du mode de combustion d'un moteur a combustion interne |
US6425373B1 (en) * | 1999-08-04 | 2002-07-30 | Ford Global Technologies, Inc. | System and method for determining engine control parameters based on engine torque |
US6880532B1 (en) | 2000-01-07 | 2005-04-19 | Ford Global Technologies, Llc | Engine operation parameter estimation method |
JP4089127B2 (ja) * | 2000-04-21 | 2008-05-28 | トヨタ自動車株式会社 | 内燃機関の制御装置 |
DE10030936A1 (de) * | 2000-06-24 | 2002-01-03 | Bosch Gmbh Robert | Verfahren zum Betreiben einer Brennkraftmaschine insbesondere eines Kraftfahrzeugs |
DE10043689A1 (de) * | 2000-09-04 | 2002-03-14 | Bosch Gmbh Robert | Verfahren zur Verlustmomentenadaption bei einer Brennkraftmaschine |
DE10049167A1 (de) * | 2000-09-27 | 2002-01-03 | Siemens Ag | Verfahren und Vorrichtung zur Einstellung der Fahrgeschwindigkeit in Fahrzeugen mit direkteinspritzender Brennkraftmaschine |
DE10048250A1 (de) * | 2000-09-29 | 2002-04-11 | Bayerische Motoren Werke Ag | Steuergerät zum Steuern eines Verbrennungsmotors mit variabel steuerbarem Ventilhub |
DE10149238A1 (de) | 2001-10-05 | 2003-04-24 | Bosch Gmbh Robert | Verfahren zum Betreiben einer Brennkraftmaschine |
GB2408353B (en) * | 2002-07-12 | 2006-01-11 | Cummins Inc | Start-up control of internal combustion engines |
EP1431555B1 (fr) | 2002-12-20 | 2014-01-22 | Honda Motor Co., Ltd. | Système et méthode de commande pour moteur à combustion interne |
JP4600932B2 (ja) * | 2006-02-21 | 2010-12-22 | 株式会社デンソー | 内燃機関の制御装置 |
US7810468B2 (en) * | 2007-06-13 | 2010-10-12 | Denso Corporation | Controller and control system for internal combustion engine |
US9163578B2 (en) * | 2008-10-15 | 2015-10-20 | Toyota Jidosha Kabushiki Kaisha | Control device for internal combustion engine |
JP2015121147A (ja) * | 2013-12-24 | 2015-07-02 | トヨタ自動車株式会社 | エンジン停止制御装置 |
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JPS5937236A (ja) | 1982-08-26 | 1984-02-29 | Nissan Motor Co Ltd | 燃料噴射時期制御方法 |
JPS62110536A (ja) | 1985-11-06 | 1987-05-21 | Toyota Motor Corp | 車両駆動系の制御装置 |
US5778856A (en) * | 1993-12-28 | 1998-07-14 | Mitsubishi Jidosha Kogyo Kabushiki Kaisha | Control device and control method for lean-burn engine |
EP0687809B1 (fr) * | 1994-06-17 | 2001-08-29 | Hitachi, Ltd. | Dispositif et méthode de commande du couple de sortie d'un moteur à combustion interne |
JPH09287513A (ja) * | 1996-02-23 | 1997-11-04 | Nissan Motor Co Ltd | エンジンのトルク制御装置 |
US5931138A (en) * | 1996-02-23 | 1999-08-03 | Nissan Motor Co., Ltd. | Engine torque control apparatus |
DE19612150A1 (de) * | 1996-03-27 | 1997-10-02 | Bosch Gmbh Robert | Steuereinrichtung für eine Benzin-Brennkraftmaschine mit Direkteinspritzung |
JP3521632B2 (ja) * | 1996-07-30 | 2004-04-19 | 日産自動車株式会社 | 内燃機関の制御装置 |
JP3680491B2 (ja) * | 1997-06-02 | 2005-08-10 | 日産自動車株式会社 | 内燃機関の制御装置 |
DE69841026D1 (de) * | 1997-06-03 | 2009-09-10 | Nissan Motor | Maschine mit Momentsteuerung |
JP3514077B2 (ja) * | 1997-06-24 | 2004-03-31 | 日産自動車株式会社 | エンジンのスロットル制御装置 |
DE69825682T2 (de) * | 1997-06-25 | 2005-01-13 | Nissan Motor Co., Ltd., Yokohama | Steuervorrichtung einer direkteinspritzenden Otto-Brennkraftmaschine |
JP3815006B2 (ja) * | 1997-12-09 | 2006-08-30 | 日産自動車株式会社 | 内燃機関の制御装置 |
-
1997
- 1997-12-15 JP JP9345144A patent/JPH11182299A/ja active Pending
-
1998
- 1998-12-14 DE DE69837189T patent/DE69837189T2/de not_active Expired - Lifetime
- 1998-12-14 EP EP98123769A patent/EP0924420B1/fr not_active Expired - Lifetime
- 1998-12-15 US US09/211,039 patent/US6145489A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9284897B2 (en) | 2012-08-31 | 2016-03-15 | Honda Motor Co., Ltd. | Intake control system for internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
JPH11182299A (ja) | 1999-07-06 |
US6145489A (en) | 2000-11-14 |
EP0924420A2 (fr) | 1999-06-23 |
DE69837189D1 (de) | 2007-04-12 |
DE69837189T2 (de) | 2007-06-21 |
EP0924420A3 (fr) | 2000-09-13 |
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